Pressure medium fluid circuit for active suspension system with variable fluid source discharge rate depending upon magnitude of stroke in relative displacement between vehicular body and suspension member

ABSTRACT

An active suspension system utilizes an acceleration exerted on a vehicle body and a stroke magnitude in relative displacement between the vehicle body and a suspension member as parameters for controlling discharge rate of pressure medium fluid from a pressure source unit. The pressure source unit is normally driven at limited discharge rate for minimizing driving power consumption. The pressure source unit is responsive to the vertical acceleration greater than a predetermined acceleration criterion and to vertical stroke magnitude greater than a predetermined stroke criterion to increase discharge rate for compensating pressure medium fluid amount to be consumed for suspension control.

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention relates generally to an active suspension system for an automotive vehicle. More particularly, the invention relates to a pressure medium fluid circuit to be adapted for the active suspension system, which achieves optimal fluid discharge performance.

2. Description of the Background Art

U.S. Pat. No. 4,702,490, issued on Oct. 27, 1987 which has been assigned to the common owner to the present invention, discloses one of typical construction of an actively controlled suspension system, in which a hydraulic cylinder defining a working chamber is disposed between a vehicular body and a suspension member rotatably supporting a vehicular wheel. The working chamber of the hydraulic cylinder is communicated with a hydraulic circuit including a pressurized working fluid source. A pressure control valve, such as a proportioning valve assembly, is disposed in the hydraulic circuit, which is connected to an electric or electronic control circuit to be controlled the valve position. The pressure control valve is controlled the valve position by a suspension control signal produced in the control circuit for adjusting pressure in the working chamber and whereby controlling suspension characteristics.

On the other hand, European Patents 0 283 004, 0 285 153 and 0 284 053 disclose technologies for controlling the suspension systems constructed as set forth above, depending upon the vehicle driving condition for suppressing rolling and/or pitching of the vehicular body.

In one of the typical construction of the hydraulic circuit includes a pressure source unit which comprises a fluid pump drivingly associated with an automotive internal combustion engine so as to be driven by the engine output torque. The fluid pump is generally rated to produce rated pressure which is selected in view of the required line pressure in a supply line for supplying the pressurized fluid to the working chamber, at the minimum revolution speed of the engine so that the working fluid pressure to be supplied to the working chamber of the hydraulic cylinder can be satisfactorily high at any engine driving range. As will be appreciated, the output pressure of the fluid pump increases according increasing of the engine revolution speed. Therefore, at high engine revolution speed range, excessive pressure in excess of a predetermined maximum line pressure is relieved via a relief valve. Therefore, the engine output can be wasted to degrade engine driving performance as a power plant for the automotive vehicle and thus degrade fuel economy.

On the other hand, in the practical operation of the active suspension system, the fluid pressure in the working chamber in the hydraulic cylinder can be maintained at constant value for maintaining a desired vehicular height, at substantially low vehicle speed range or while the vehicle is not running. Despite this fact, the prior proposed hydraulic circuits for the actively controlled suspension systems supply the rated pressure of the fluid pump which should be higher than a minimum line pressure required for adjustment of the fluid pressure in the working chamber.

Improvement in the hydraulic circuit for the prior proposed active suspension system has been proposed in the co-pending U.S. patent application Ser. No. 331,602, filed on Mar. 31, 1989, which application has been commonly assigned to the common assignee to the present invention. The corresponding invention to the above-identified co-pending U.S. Patent Application has been published as Japanese Patent First (unexamined) Publication (Tokkai) Heisei 1-249509, published on Oct. 4, 1989. The prior invention has been directed to a hydraulic circuit for an actively controlled suspension system which employs first and second pressure relief valves disposed in a hydraulic pressure source circuit for relieving excessive pressure. The second pressure relief valve is provides a lower relief pressure than that of the first pressure relief valve. Means for selectively connecting and disconnecting the second pressure relief valve is disposed in the hydraulic pressure source circuit at an orientation upstream of the second pressure relief valve. The means is positioned at shut-off position to disconnect the second pressure relief valve when a vehicle traveling speed is higher than a predetermined speed. The means is responsive to the vehicle speed lower than the predetermined speed for establishing connection between a pressurized fluid source to the second relief valve for relieving the pressure at lower level than that established when the vehicle speed is higher than the predetermined speed.

Furthermore, the prior proposed invention includes a pilot pressure operated one-way check valve in a drain line for regulating line pressure to be supplied to a pressure control valve which adjusts fluid pressure in a working chamber in a hydraulic cylinder disposed between a vehicle body and a suspension member rotatably supporting a road wheel, by draining excessive line pressure. Similar hydraulic circuit constructions have also been disclosed in European Patent First Publications Nos. 0 318 721, 0 318 932, for example.

In the prior proposed active suspension systems, the fluid pressure is supplied from a fluid pump which is driven by an automotive internal combustion engine. As can be appreciated, such type of the fluid pump is variable of discharge rate depending upon the engine revolution speed. In order to prevent pulsation in the line pressure, a pressure regulating means is provided in the pressure supply network. On the other hand, when acceleration of stroke in relative bounding and rebounding motion of the vehicle body and the suspension member, increased discharge rate of the fluid pump is required so as to compensate the relatively large amount of working fluid supplied and drained into and from a working cylinder. Japanese Patent First (unexamined) Publication (Tokkai) Showa 63-251313 has discloses the pressure supply system having capability of adjustment of the discharge rate of the fluid pump depending upon relatively large magnitude of bounding and/or rebounding acceleration.

The proposed system is particularly advantageous when the vehicle is in the parking, resting or not running state because of smaller discharge rate of the fluid pump for smaller power loss in the engine. On the other hand, the proposed system is so designed as to command increasing of the discharge rate in response to large magnitude of bounding and rebounding acceleration. However, the signal representative of bounding and rebounding magnitude does not necessarily correspond to the fluid flow rate to be consumed in the active suspension system. Therefore, the discharge rate of the fluid pump as controlled by the command generated in response to large magnitude of bounding and rebounding acceleration cannot precisely correspond to that required in the active suspension system. Therefore, the line pressure tends to become excessively high to lead wasting of the engine output power and excessively low to lead in sufficient suspension adjusting performance.

SUMMARY OF THE INVENTION

Therefore, it is an object of the present invention to provide a pressure supply network which can solve the drawback in the prior art and thus optimize the fluid pump operation at any vehicle driving condition without causing degradation of pressure supply response characteristics.

In order to accomplish aforementioned and other objects, an active suspension system, according to the present invention, utilizes an acceleration exerted on a vehicle body and a stroke magnitude in relative displacement between the vehicle body and a suspension member as parameters for controlling discharge rate of pressure medium fluid from a pressure source unit. The pressure source unit is normally driven at limited discharge rate for minimizing driving power consumption. The pressure source unit is responsive to the acceleration greater than a predetermined acceleration criterion end to vertical stroke magnitude greater than a predetermined stroke criterion to increase discharge rate for compensating pressure medium fluid amount to be consumed for suspension control. According to one aspect of the invention, a fluid supply system for an active suspension system for supplying fluid pressure for a hollow working cylinder via a pressure control valve for adjusting suspension characteristics in order to suppress vehicular attitude change and absorb road shock vibration, the system comprises:

a pressurized fluid source unit for circulating pressurized fluid through a fluid circuit extending via the pressure control valve and the working cylinder;

a sensor means for monitoring relative displacement between a vehicular body and a suspension member rotatably supporting a road wheel for producing a relative displacement magnitude indicative signal;

first means for deriving a predicted fluid flow amount through the fluid circuit on the basis of the relative displacement indicative signal to produce a predicted fluid flow amount indicative signal;

second means for detecting a magnitude of relative displacement greater than or equal to a predetermined displacement stroke criterion to produce a large stroke indicative signal; and

third means for deriving fluid supply mount from the pressurized fluid source unit on the basis of the predicted fluid flow amount for controlling the pressurized fluid source unit in order to adjust the supply amount of fluid toward the derived fluid supply amount, the third means being responsive to the large stroke indicative signal for increasing the supply amount.

The third means may maintain the increased supply amount for a given period of time after termination of the large stroke indicative signal. The second means derives an average value of the displacement magnitude indicative signal and derives a difference between the average value and the displacement indicative signal for producing the large stroke indicative signal when the difference is greater than a predetermined value representative of the displacement stroke criterion. In the preferred process, the third means extract a predetermined frequency range of signal component in the displacement magnitude indicative signal and derives a difference between the extracted signal level and the signal level of the displacement magnitude indicative signal for producing the large stroke indicative signal when the difference is greater than a predetermined value representative of the displacement stroke criterion.

The fluid circuit may include a supply line for supplying the pressurized fluid to the pressure control valve and a drain line for recirculating the pressurized fluid to the pressurized fluid source unit, and the pressurized fluid source unit including a by-pass line connecting between the supply line and the drain line by-passing the pressure control valve and a flow control valve means disposed within the by-pass line for adjusting pressurized fluid recirculation rate through the by-pass line for adjusting fluid supply amount to the pressure control valve to the derived amount. The pressurized fluid source unit may comprise a first pump having a first greater discharge rate and a second pump having a second smaller discharge rate, the flow control valve means selectively connect the first and second pump to the drain line via the by-pass line. In such case, the first and second pumps may be coupled with an automotive engine to be driven by the output thereof. Respective of the first and second pumps may be variable of fluid discharge rate depending upon revolution speed thereof which is variable depending upon revolution speed of the engine.

The fluid supply control system may further comprise a pump speed sensor for monitoring pump speed to produce a pump speed indicative signal, and the third means derives the fluid supply amount on the basis of the predicted fluid flow amount and the pump speed as represented by the pump speed indicative signal. In the preferred construction, the sensor means comprises a stroke sensor for monitoring magnitude of stroke of bounding and rebounding activity of the vehicle to produce a stroke indicative signal. The first means may extract a predetermined frequency range of signal component in the stroke indicative signal for processing the extracted signal component for deriving the predicted fluid flow amount. Preferably, the first means may includes a band-pass filter having a pass band corresponding to the predetermine frequency range.

Furthermore, the fluid supply control system further comprises a pump speed sensor for monitoring revolution speed of a pump incorporated in the pressurized fluid source unit to produce a pump speed indicative signal, and the third means derives the fluid supply amount on the basis of the predicted fluid flow amount and the pump speed as represented by the pump speed indicative signal, and modifies the fluid supply amount for a given rate in response to the large stroke indicative signal. In the practical implementation, the third means may select basic discharge characteristics of the pump on the basis of daid predicted fluid flow amount and the pump speed and modifies the discharge characteristics in response to the large stroke indicative signal.

BRIEF DESCRIPTION OF THE DRAWINGS

The present invention will be understood from the detailed description given herebelow and from the accompanying drawings of the preferred embodiments of the invention, which, however, should not be taken for limiting the invention to the specific embodiments, but are for explanation and understanding only.

In the drawings:

FIG. 1 is a diagrammatical illustration of the overall construction of the preferred embodiment of an active suspension system, according to the present invention, in which the preferred embodiment of a proportioning valve assembly is employed as a pressure control valve;

FIG. 2 is a sectional view of the preferred embodiment of the pressure control valve according to the present invention;

FIG. 3 is a circuit diagram of the first embodiment of a hydraulic circuit which is applicable for the active suspension system according to the present invention;

FIG. 4 is a chart showing relationship between an electric current value of a control signal to be supplied for an actuator of the pressure control valve and a working fluid pressure supplied to a working chamber of a hydraulic cylinder; and

FIG. 5 is a section of an operational one-way check valve employed in the hydraulic circuit of FIG. 3;

FIG. 6 is a chart showing discharge characteristics versus pump speed in a pressure unit employed in the first embodiment of the hydraulic circuit of FIG. 3;

FIG. 7 is a block diagram of a discharge rate control circuit employed for controlling discharge rate of the pressure unit in the first embodiment of the hydraulic circuit of FIG. 3;

FIG. 8 is a chart showing variation of stroke and an integrated value thereof as integrated by an integrator employed in the discharge rate control circuit of FIG. 7;

FIG. 9 is a flowchart showing process in a routine for setting operational mode of the pressure unit;

FIG. 10 is a flowchart showing process of detection of a vertical stroke magnitude greater than a predetermined stroke criterion;

FIG. 11 is a timing chart showing variation of vertical stroke;

FIG. 12 is a circuit diagram of the second embodiment of the hydraulic circuit in the active suspension system;

FIG. 13 is a block diagram of the discharge rate control circuit to be employed for controlling discharge rate of the pressure unit in the second embodiment of the hydraulic circuit of FIG. 12;

FIG. 14 is a chart showing variation of fluid discharge rate of a pressure unit employed in the second embodiment of the hydraulic circuit of FIG. 12;

FIG. 15 is a flowchart showing process of mode selection to be taken place in the second embodiment of the hydraulic circuit of FIG. 12;

FIG. 16 is a flowchart showing process of detection of a vertical stroke greater than a stroke criterion;

FIGS. 17 and 18 are flowcharts showing modified processes of mode selection and detection of excessive vertical stroke to be performed in hydraulic circuit of the invention; and

FIG. 19 is a chart showing variation of discharge rate at respective flow rate mode to be selected in terms of predicted flow rate Q_(AA) and the pump speed N.

DESCRIPTION OF THE PREFERRED EMBODIMENT

Referring now to the drawings, particularly to FIG. 1, the preferred embodiment of an active suspension system, according to the present invention, is designed to generally perform suspension control for regulating vehicular height level and vehicular attitude by suppressing relative displacement between a vehicular body 10 and suspension members 24FL, 24FR, 24RL and 24RR provided in front-left, front-right, rear-left and rear-right suspension mechanism 14FL, 14FR, 14RL and 14RR and rotatably supporting front-left, front-right, rear-left and rear-right wheels 11FL, 11FR, 11RL and 11RR. The suspension member will be hereafter represented by the reference numeral "24" as generally referred to. Similarly, the suspension mechanism as generally referred to will be hereafter represented by the reference numeral "14" Respective front-left, front-right, rear-left and rear-right suspension mechanisms 14FL, 14FR, 14RL and 14RR have hydraulic cylinders 26FL, 26FR, 26RL and 26RR which will be represented by the reference numeral "26" as generally referred to.

Each of the hydraulic cylinder 26 is disposed between the vehicular body 10 and the suspension member 24 to produce a damping force for suppressing relative displacement between the vehicular body and the suspension member. The hydraulic cylinder 26 generally comprises an essentially enclosed cylindrical cylinder body 26a defining therein an enclosed chamber. A thrusting piston 26c is thrustingly and slidably disposed within the enclosed chamber of the hydraulic cylinder 26 for defining in the latter a working chamber 26d and a reference pressure chamber 26e. The working chamber 26d may be communicated with the reference pressure chamber 26e via an orifice formed through the piston for fluid communication therebetween in an substantially restricted amount. The piston 26c is connected to the associated one of suspension member 24 via a piston rod 26b. A suspension coil spring 36 employed in the shown type of the suspension system is not required a resilient force in a magnitude required in the ordinary suspension system and only required the resilient force necessary for maintaining the vehicular body about the suspension member.

The working chamber 26d of the hydraulic cylinder 26 is connected one of pressure control valves 28FL, 28FR, 28RL and 28RR via a pressure control line 38. The pressure control valve 28FL, 28FR, 28RL and 28RR will be hereafter represented by the reference numeral "28" as generally referred to. The pressure control valve 28 is, in turn, connected to a pressure source unit 16 via a supply line 35 and a drain line 37. A branch circuit is provided for connecting the pressure control line 38 to a pressure accumulator 34 via a flow restricting means, such as an orifice 32. Another pressure accumulator is provided in the supply line 35 for accumulating the excessive pressure generated in the pressure source unit 16.

The pressure control valves 28 comprise, though it is not clearly shown in FIG. 1, electrically or electromagnetically operable actuators (reference is made to FIG. 2), such as a proportioning solenoids. The actuators are connected to a microprocessor based control unit 22. The control unit 22 is connected to a plurality of vehicular height sensors 21 which are disposed in respectively associated suspension mechanism and designed for monitoring relative position of the vehicular body 10 and the relevant suspension member 24 to produce a vehicular height level indicative signals h₁, h₂, h₃ and h₄. The control unit 22 is also connected to a lateral acceleration sensor, a longitudinal acceleration sensor and so forth to receive the vehicle driving condition indicative parameters. In FIG. 3, the lateral and longitudinal acceleration sensors will be generally referred to as "acceleration sensor" and generally represented by reference numeral 23. Based on these control parameters, including the height level indicative signals, a lateral acceleration indicative signal G_(y) generated by the lateral acceleration sensor, a longitudinal acceleration indicative signal G_(x) generated by the longitudinal acceleration sensor, and so forth, the control unit performs anti-rolling, anti-pitching and bouncing suppressive suspension controls.

Practical implementation of the suspension control have been disclosed in the various prior proposed applications. For example, publications and issued patents, all of which are commonly owned or assigned to the owner or assignee of the present invention, and for which a pressure control valve unit according to the present invention is applicable, are listed herebelow.

U.S. patent application Ser. No. 052,934, filed on May 22, 1989, which has now been issued as U.S. Pat. No. 4,903,983, on Feb. 27, 1990:

U.S. patent application Ser. No. 059,888, filed on June 9, 1987, 1987, corresponding European Patent Application has been published as First Publication No. 02 49 209:

U.S. patent application Ser. No. 060,856, filed on June 12, 1987, corresponding European Patent Application has been published as First Publication No. 02 49 227:

U.S. patent application Ser. No. 060,909, filed on June 12, 1987, now issued as U.S. Pat. No. 4,909,534 on Mar. 20, 1990:

U.S. patent application Ser. No. 060,911, filed on June 12, 1987, which has now been issued as U.S. Pat. No. 4,801,155, on Jan. 31, 1989:

U.S. patent application Ser. No. 176,246, filed on Mar. 31, 1988, the corresponding European Patent Application has been published as First Publication No. 02 85 153, now issued as U.S. Pat. No. 4,888,696 on Dec. 19, 1989:

U.S. patent application Ser. No. 178,066, filed on Apr. 5, 1988, which has now been issued as U.S. Pat. No. 4,848,790, on July 18, 1989, and the corresponding European Patent Application has been published as First Publication No. 02 86 072:

U.S. patent application Ser. No. 167,835, filed on Mar. 4, 1988, which has now been issued as U.S. Pat. No. 4,865,348, on Sept. 12, 1989:

U.S. patent application Ser. No. 244,008, filed on Sept. 14, 1988, now issued as U.S. Pat. No. 4,938,499 on July 3, 1990:

U.S. patent application Ser. No. 255,560, filed on Oct. 11, 1988, now issued as U.S. Pat. No. 4,943,084 on July 24, 1990:

U.S. patent application Ser. No. 266,763, filed on Nov. 3, 1988, corresponding European Patent Application has been published under First Publication No. 03 18 721, now issued as U.S. Pat. No. 4,967,360 on Oct. 30, 1990:

U.S. patent application Ser. No. 261,870, filed on Oct. 25, 1988:

U.S. patent application Ser. No. 263,764, filed on Oct. 28, 1988, corresponding European Patent Application has been published under First Publication No. 03 14 164, now issued as U.S. Pat. No. 4,905,152 on Feb. 27, 1990:

U.S. patent application Ser. No. 277,376, filed on Nov. 29, 1988, corresponding European Patent Application has been published under First Publication No. 03 18 932, now issued as U.S. Pat. No. 4,919,440 on Apr. 24, 1990:

U.S. patent application Ser. No. 303,338, filed on Jan. 26, 1989, corresponding German Patent Application has been published under First Publication No. 39 02 312:

U.S. patent application Ser. No. 302,252, filed on Jan. 27, 1989:

U.S. patent application Ser. No. 310,130, filed on Mar. 22, 1989, corresponding German Patent Application has been published under First Publication No. 39 04 922, now issued as U.S. Pat. No. 4,973,079 on Nov. 27, 1990:

U.S. patent application Ser. No. 327,460, filed on Mar. 22, 1989, corresponding German Patent Application has been published under First Publication No. 39 10 030, now issued as U.S. Pat. No. 4,911,469 on Mar. 27, 1990:

U.S. patent application Ser. No. 303,339, filed on Jan. 26, 1989, now issued as U.S. Pat. No. 4,948,165 on Aug. 14, 1990:

U.S. patent application Ser. No. 331,602, filed on Mar. 31, 1989, now issued as U.S. Pat. No. 4,911,468:

U.S. patent application Ser. No. 331,653, filed Mar. 31, 1989, corresponding German Patent Application has been published under First Publication No. 39 10 445, now issued as U.S. Pat. No. 4,911,470 on Mar. 27, 1990:

U.S. patent application Ser. No. 364,477, filed on June 12, 1989, corresponding European Patent Application has been published under First Publication No. 03 45 816:

U.S. patent application Ser. No. 365,468, filed on June 12, 1989, corresponding European Patent Application has been published under First Publication No. 03 45 817:

U.S. patent application Ser. No. 422,813, filed on Oct. 18, 1989, now issued as U.S. Pat. No. 4,961,595 on Oct. 9, 1990:

U.S. patent application Ser. No. 454,785, filed on Dec. 26, 1989, now issued as U.S. Pat. No. 4,982,979 on Jan. 8, 1991:

The following above listed U.S. Patent Applications are pending as of Apr. 30, 1991:

U.S. patent application Ser. No. 059,888, filed on June 9, 1987;

U.S. patent application Ser. No. 060,856, filed on June 12, 1987;

U.S. patent application Ser. No. 303,338, filed on Jan. 26, 1989;

U.S. patent application Ser. No. 302,252, filed on Jan. 27, 1989;

U.S. patent application Ser. No. 364,477, filed on June 12, 1989;

U.S. patent application Ser. No. 365,468, filed on June 12, 1989;

The disclosures of the hereabove listed prior applications, publications and patents are herein incorporated by reference.

While the specific sensors, such as the vehicle height sensors which comprise strike sensor, the lateral acceleration sensor and the longitudinal acceleration sensor, it is possible to replace or add any other sensors which monitors vehicle driving parameter associated with the suspension control. The lateral acceleration sensor may be replaced with a steering angle sensor for monitoring steering behavior for assuming lateral force to be exerted on the vehicular body. The indicative of the steering angular displacement may be used in combination of a vehicular speed data since vehicular speed may influence for rolling magnitude of the vehicle during steering operation.

As shown in FIG. 2 in detail, the pressure control valve 28 comprises a proportioning valve assembly and is designed to be controlled by an electric current is as a control signal supplied from the control unit 22 for varying valve position according to variation of the current value of the control signal. Generally, the pressure control valve 28 controls magnitude of introduction and draining of pressurized fluid into and from the working chamber 26d for adjusting the pressure in the working chamber. As will be appreciated, since the adjusted fluid pressure in the working fluid determines damping force to be created in response to relative displacement between the vehicle body 10 and the suspension member 24. Mode of the suspension mechanism is varied according to variation of the fluid pressure in the working chamber between a predetermined hardest mode to most soft mode.

In the construction of the pressure control valve shown in FIG. 2, the pressure control valve 28 includes a valve housing 42. The valve housing 42 defines a valve bore 44 which is separated in to a valve chamber 42L and a control chamber 42U by means of a partitioning wall 46. The partitioning wall 46 is formed with a communication path opening 46A for communication between the control chamber 42U and the valve chamber 42L. As seen from FIG. 2, the control chamber 42U and the valve chamber 42L are arranged in alignment to each other across the communication path opening 46A. In parallel to a section of the partitioning wall 46 extending perpendicular to the axis of the valve chamber 42L and the control chamber 42U, a fixed orifice defining partitioning member 50 is provided. The partitioning member 50 defines a throttling orifice which is oriented substantially in alignment with the communication path opening 46A. The partitioning wall 46 and the partitioning member 50 are cooperative for defining a pilot chamber PR therebetween.

A valve spool 52 is thrustingly and slidingly disposed within the valve chamber 42L. The valve spool 52 defines an upper feedback chamber FU between the tip end thereof and the partitioning member 50. The valve spool 52 also defines a lower feedback chamber FL between the other tip end thereof and the bottom of the valve chamber 42L. Offset springs 60U and 60L are disposed within the upper and lower feedback chambers FU and FL, which offset springs exerts spring force to the valve spool 52 for resiliently restricting movement of the latter. Resilient force of the offset springs 60U and 60L are so set as to balance to place the valve spool 52 at a neutral position, when the fluid pressure in the upper and lower feedback chambers FU and FL balances to each other. The valve chamber 42L is communicated with the supply line 35 via a supply port 54s, the drain line 37 via a drain port 54r and the drain port 54r and a pressure control line 38 via a control port 54c, which supply port, drain port and control port are defined in the valve housing 42. The valve spool 52 at the aforementioned neutral position, blocks fluid communication of the pressure control chamber PC with any of the supply port 54s and the drain port 54r. As a result, as long as the valve spool 52 is maintained at the neutral position, overall fluid force in the hydraulic circuit downstream of the pressure control valve, which circuit includes the working chamber 26d of the hydraulic cylinder 26 is held constant.

The valve spool 52 is formed with lands 52a and 52b connected to each other via smaller diameter bar-like section 52e. The land 52a is oriented adjacent the lower feedback chamber FL so as to subject the tip end to the fluid pressure in the lower feedback chamber. Similarly, the land 52b is oriented adjacent the upper feedback chamber FU so as to subject the tip end to the fluid pressure in the upper feedback chamber. The bar-like section 52e between the lands 52a and 52b is cooperative with the peripheral wall of the valve chamber 42L in order to define therebetween a pressure control chamber PC. A fluid flow path 52d is formed through the valve spool 52. The fluid flow path 52d has one end communicated with the pressure control chamber PC and the other end communicated with the lower feedback chamber FL. A fixed flow restricting orifice 52f is formed in the fluid flow path 52d for restricting fluid flow therethrough.

A poppet valve member 48 is disposed within the control chamber 42U for thrusting movement therein. The poppet valve member 48 has a valve head 48a of an essentially conical configuration. The valve head 48a opposes to the communication path opening 46A of the partitioning wall 46. The poppet valve member 48 is operably associated with a proportioning solenoid assembly 29 as the actuator. The proportioning solenoid assembly 29 comprises a housing 62 rigidly secured on the valve housing 42 and defining an internal space 64 to receive therein a plunger 66. The plunger 66 has a plunger rod 66A. The tip end of the plunger rod 66A is kept in contact with the tip end of the poppet valve member 48 remote from the valve head 48a. Therefore, the poppet valve member 48 is axially driven by means of the plunger 66 to control the path area in the communication path opening 46A according to the position of the tip end of the plunger rod 66A. Adjusting of the path area in the communication path opening 46A results in variation of fluid pressure to be introduced into the pilot chamber PR.

In order to control the position of the plunger 66 with the plunger rod 66A, a proportioning solenoid coil 68 is housed within the housing 62 and surrounds the plunger 66. The interior space of the housing 62 is connected to the control chamber 42U for fluid communication therebetween. The plunger 66 is formed with a fluid path 66B for fluid communication between upper and lower sections of the interior space. Therefore, the fluid pressure in the upper and lower sections of the interior space of the housing 62 is held equal to the pressure in the control chamber 42U. This cancels fluid pressure to be exerted on the poppet valve and the plunger so that the position of the tip end of the plunger rod 66A can be determined solely depending upon the magnitude of energization of the proportioning solenoid coil 68.

As seen from FIG. 2, the poppet valve member 48 has a cylindrical larger diameter section 48b for separating the control chamber 42U into upper section and lower section 42Uu and 42Ul. The upper and lower sections 42Uu and 42Ul are communicated with the drain port 54r via a pilot return path PT. A multi-stage orifice Pr is provided in the pilot return path PT for restricting fluid flow therethrough. The multi-stage orifice Pr comprises a plurality of strips formed with through openings and is so designed that one of the orifice oriented at most upstream side is mainly effective for restricting fluid flow when fluid flowing therethrough is steady flow and that all of the orifices of respective strips are equally effective for restricting fluid flow when fluid flow therethrough is disturbed and not steady. Therefore, as will be appreciated herefrom, the multi-stage orifice Pr employed in the shown embodiment serves to provide greater fluid flow restriction against non-steady or disturbed fluid flow than that for the steady flow. As seen from FIG. 2, the multi-stage orifice Pr is provided upstream of the upper and lower sections 42Uu and 42Ul. On the other hand, a fixed throttling orifice Pd is provided at an orientation downstream of the lower section 42Ul and upstream of the upper section 42Uu. Similarly, the pilot chamber PR is communicated with the supply port 54s via a pilot path PP. A multi-stage orifice Qp which has similar construction and flow restricting function to that of the multi-stage orifice Pr is provided in the pilot path PP.

A fixed throttle orifice Pro is also provided in the drain port 54r for restricting fluid flow therethrough. The diameter of the fluid path at the orifice Pro is so selected as to create great flow restriction against pulsatile fluid flow cyclically varying the fluid pressure at a frequency approximately 1 Hz.

As can be seen from FIG. 2, the pressure control valve 28 is so arranged as to direct the axis of the valve bore 44 parallel to the longitudinal axis of the vehicle body. The longitudinal acceleration to be exerted on the vehicular body is much smaller than the lateral acceleration and vertical acceleration exerted on the vehicle body. Therefore, by arranging the pressure control valve 28 so that the poppet valve 48 and the valve spool 52 thrustingly move in longitudinal direction, influence of the externally applied acceleration can be minimized.

FIG. 3 shows detailed circuit construction of one example of hydraulic circuit which is applicable for the shown embodiment of the active suspension system, according to the present invention. The hydraulic circuit includes a fluid pressure source circuit which includes the pressure source unit 16. The pressure source unit 16 includes the pressure unit 16b which comprises a fluid pump, and is connected to a fluid reservoir 16a via a suction pipe 201. The fluid pump unit 16b is associated with an automotive engine 200 so as to be driven by the output torque of the latter output from an engine output shaft 200a. In the shown embodiment, the fluid pump unit 16b comprises a plunger pump having a plurality of cylinders. Among the plurality of cylinders, a first group of cylinders is constituted of every other cylinders and forms a first pump 16_(Qa), and a second group of cylinders is constituted of another every other cylinders and forms a second pump 16_(Qb). The discharge rate of the first pump 16_(Qa) is set to be greater than that of the second pump 16_(Qb). The discharge characteristics versus the engine speed dependent pump speed of respective of the first and second pumps 16_(Qa) and 16_(Qb) are illustrated in FIG. 6.

The outlet of the first pump 16_(Qa) is connected to the supply port 54s of the pressure control valve 28 via a branched supply line 35a and a common supply line 35c. Similarly, the outlet of the second pump 16_(Qb) is connected to the supply port 54a of the pressure control valve 28 via a branched supply line 35b and the common supply line 35c. One-way check valves 220a and 220b are disposed in respective of the branched supply lines 35a and 35b. On the other hand, a pressure accumulator 27 for absorbing pulsatile are disposed in the common supply line 35c. A one-way check valve 204 is disposed in the common supply line 35c at the position upstream of the junction between the pressure accumulators 27 and the supply line 35.

A first flow control line 205a is also connected to the branched supply line 35a at one end. The other end of the first flow control line 205a is communicated with the fluid reservoir 16a. An electromagnetic flow control valve 206 is disposed in the first flow control line 205a. The electromagnetic flow control valve 205 has a first inlet port 206a connected to the branched supply line 35a via the first flow control line 205a. Similarly, a second pressure relief line 205b is connected to the branched supply line 35b at one end. The other end of the second flow control line 205b is communicated with the fluid reservoir 16a. The electromagnetic flow control valve 206 is also disposed in the second flow control line 205b. The electromagnetic flow control valve 206 has a second inlet port 206b connected to the branched supply line 35b via the second pressure relief line 205b. The electromagnetic flow control valve 206 also has an output port 206c communicated with the fluid reservoir 16a via a return line 205c.

The electromagnetic flow control valve 206 includes an electromagnetically operable solenoid 206d for switching valve position of the flow control valve in response to a flow control signal CS supplied from a fluid supply controller 400 which will be discussed in detail later. In the shown embodiment, the flow control signal CS is variable between HIGH level and LOW level for commanding variation of the position of the electromagnetic flow control valve 206. The solenoid 206d is responsive to the LOW level flow control signal CS to place the electromagnetic flow control valve 206 at a position where fluid communication between the first inlet port 206a and the outlet port 206c is established and the fluid communication between the second inlet port 206b and the outlet port 206c is blocked. At this valve position, large proportion of or most part of the pressurized fluid discharged from the first pump 16_(Qa) is directly drained to the fluid reservoir 16a via the first flow control line 205a, the electromagnetic flow control valve 206 and the return line 205c. On the other hand, the solenoid 206d is responsive to the HIGH level flow control signal CS to place the electromagnetic flow valve 206 at a position where fluid communication between the second inlet port 206b and the outlet port 206c is established and the fluid communication between the first inlet port 206a and the outlet port 206c is blocked. At this valve position, large proportion of or most part of the pressurized fluid discharged from the second pump 16_(Qb) is directly drained to the fluid reservoir 16a via the second flow control line 205b, the electromagnetic flow control valve 206 and the return line 205c. As can be appreciated, since the first pump 16_(Qa) has greater discharge rate than that of the second pump 16_(Qb), greater fluid flow rate is established when the valve is in the latter mentioned position. In the following disclosure, the operational mode of the electromagnetic flow control valve 206 at the former valve position in which the first inlet port and the outlet port are communication, will be hereafter referred to as "smaller flow rate mode" and at the latter valve position, in which the second inlet port and the outlet port are communicated, will be hereafter referred to as "greater flow rate mode".

In parallel to the electromagnetic valve 206, a pressure regulator valve 207 is provided for regulating line pressure in the supply line 35. The pressure regulator valve 207 is connected to the supply line 35 at an orientation downstream of the junction of the first and second branched supply lines 35a and 35b and upstream of the one-way check valve 204. The pressure regulator valve 207 is so designed to regulate the line pressure in the supply line at a predetermined set pressure.

On the other hand, an operational one-way check valve 300 is disposed between the sections 37a and 37b of the drain line 37. The operational one-way check valve 300 is also connected to the supply line 35 downstream of the one-way check valve 204 to receive therefrom the pressure in the supply line as a pilot pressure, via a pilot line 208. The operational one-way check valve 300 is designed to be maintained at open position as long as pilot pressure introduced from the supply line 35 at the orientation downstream of the one-way check valve 204 is held higher than a predetermined pressure. At the open position, the operational one-way check valve maintains fluid communication between the inlet side and outlet side thereof so that the working fluid in the drain line 37 may flow therethrough to the reservoir tank 16a. On the other hand, the operational one-way check valve 300 is responsive to the working fluid pressure in the supply line downstream of the one-way check valve 204 serving as the pilot pressure dropping below the predetermined pressure level to be switched into shut-off position. At the shut-off position, the operational one-way check valve 300 blocks fluid communication between the drain port 54r of the pressure control valve 28 and the reservoir tank 16a. In the shown embodiment, the predetermined pressure is set at a pressure corresponding to the neutral pressure of the pressure control valve unit 28.

For the section 37b of the drain line 37, an additional pressure accumulator is traditionally provided. The additional pressure accumulator is arranged for absorbing back pressure to be generated by flow resistance in the drain line 37.

An oil cooler is generally disposed in the drain line 37 for cooling the working fluid returning to the reservoir tank 16a.

FIG. 5 shows the detailed construction of the preferred embodiment of the operational one-way check valve 300 to be employed in the preferred embodiment of the active suspension system according to the present invention. As shown in FIG. 5, the operational one-way check valve 300 comprises a valve housing 302 formed with an inlet port 304, an outlet port 306 and a pilot port 308. The valve housing 302 defines a valve bore 310. The valve bore 310 comprises a larger diameter section 312, in which a poppet valve 314 is thrustingly disposed, and a smaller diameter section 316, in which a valve spool 318 is disposed. The pilot port 308 is communicated with the supply line 35 between the one-way check valve 204 and the pressure control valve unit 28FL 28FR, 28RL and 28RR, via the pilot line 208. The pilot port 308 is, on the other hand, communicated with the smaller diameter section 316 to supply the line pressure of the supply line 35 at the orientation downstream of the one-way check valve 204 as the pilot pressure P_(P). On the other hand, the inlet port 304 is communicated with the drain port 54r of the pressure control valve unit 28 via a section 37b of the drain line 37. The inlet port 304 communicates with the smaller diameter section 316 via an annular groove 324 formed on the inner periphery of the valve housing 302. The outlet port 306 is communicated with the fluid reservoir 16a via a section 37a of the drain line 37 and, in turn, communicated with the larger diameter section 312 via an annular groove 326 formed on the inner periphery of the valve housing 302. As seen from FIG. 5, the annular grooves 324 and 326 are oriented in side-by-side relationship with leaving a radially and inwardly projecting land 328. The land 328 has a shoulder 330.

The valve spool 318 and the poppet valve 314 are cooperated with each other to define therebetween a control chamber 334 which communicates with the inlet port 304 and the outlet port 306. On the other hand, the valve spool 318 also defines a pilot chamber 336 at a side remote from the control chamber 334. The poppet valve 314 defines a pressure setting chamber 338 at a side remote from the control chamber 334. The pressure setting chamber 338 is communicated with the outlet port 306 via a path 340. A set spring 342 is disposed within the pressure setting chamber 338 for normally exerting a spring force to the poppet valve 314. In the preferred embodiment, the set spring 342 is provided a set force which corresponds the neutral pressure P_(N) of the pressure control valve unit 28.

The valve spool 318 has a valve body 320 and a valve stem 322 projecting from the valve body toward the poppet valve 314. The tip end of the valve stem 322 contacts with the mating surface of the poppet valve 314. The poppet valve 314 has an annular shoulder 332 mating with the shoulder of the land 330.

With the construction set forth above, the operational one-way check valve 300 operates as both of the pressure relief valve for relieving the excessive pressure in the drain line and one-way check valve. The relief pressure of the poppet valve 314 can be illustrated by the following balancing equation:

    F.sub.0 =P.sub.p0 ×A

where

F₀ is the set pressure of the set spring 342;

A is an effective area of the spool; and

P_(p0) is a relief pressure.

Here, assuming that the pressure Pi at the inlet port 304 is greater than or equal to the pilot pressure P_(p) at the pilot chamber 336, the valve spool 318 is shifted away from the poppet valve 314 so that the pilot pressure P_(p) in the pilot chamber 336 is not active on the valve position of the poppet valve. In such case, the poppet valve 314 operates purely as the pressure relief valve for relieving excessive pressure. At this time, the force balance as illustrated by:

    Pi×A=P.sub.p0 ×A

can be established. Therefore, as long as the fluid pressure at the inlet port 304 is higher than the relief pressure P_(p0), the shoulder 332 of the poppet valve 314 is held away from the shoulder 330 of the land 328 so as to permit fluid flow through the outlet port 306 and the section 37a of the drain line 37 to the fluid reservoir 16a. On the other hand, when the pressure at the inlet port 304 is lower than or equal to the relief pressure P_(p0), then, the spring force of the set spring 342 overcomes the fluid pressure to establish contact between the mating shoulders 332 and 330 to block fluid communication between the control chamber 334 and the outlet port 306.

On the other hand, when the pressure Pi at the inlet port 304 is lower than the pilot pressure P_(p) in the pilot chamber 336, the valve spool 318 is shifted toward the poppet valve 314 to contact with the latter at the tip end of the valve stem 322. At this time, the force to depress the valve stem 322 onto the poppet valve 314 can be illustrated by (P_(p) -_(Pi))×A. At this time, the pressure Pi introduced into the control chamber 334 via the inlet port 304 is canceled as an internal pressure. Therefore, the pressure balance at the poppet valve 314 can be illustrated by:

    F.sub.0 +kx=P.sub.p ×A

where

k is a spring coefficient of the set spring 342; and

x is a stroke of the poppet valve 314.

From the balancing equations give hereabove, the operational check valve 300 becomes open when the pilot pressure P_(p) is higher than the relief pressure P_(p0) and is held at shut-off position while the pilot pressure is held lower than the relief pressure.

In the hydraulic circuit set forth above, the fluid in the pump 16 is driven by the engine 200 to discharge pressurized working fluid while the engine is running. The pressurized fluid discharged from the outlet of the fluid pump 16 is fed to the pressure control valve 28 via the supply line 35 including the one-way check valve 204. When the pressure control valve 28 is shifted to established fluid communication between the supply port 54s and the pressure control port 54c from the valve position shown in FIG. 2, the pressurized working fluid passes the pressure control valve 28 and introduced into the working chamber 26d of the hydraulic cylinder 26. On the other hand, when the pressure control valve 28 is shifted to block fluid communication between the supply port 54s and the pressure control chamber PC, the fluid pressure in the supply line 35 increases. When the line pressure in the supply line 35 becomes higher than or equal to the set pressure of the pressure relief valve 207 in the pressure relief line, the excessive pressure is fed to the drain line 37 via the pressure relief valve 207 and thus returned to the reservoir tank 16a.

The fluid pressure in the supply line 35 is also fed to the operational one-way check valve 300 via a pilot line 208. As set forth, the operational one-way check valve 300 is placed at open position as long as the pilot pressure introduced through the pilot line 300a is held higher than or equal to the set pressure thereof. Therefore, fluid communication between the pressure control valve 28 and the reservoir tank 16a is maintained. At this position, the working fluid is thus returned to the reservoir tank 16a via the drain line 37 via the operational one-way check valve 300 and the oil cooler (not shown) provided in the drain line 37.

The operational one-way check valve 300, even at the open position, serves as a resistance to the fluid flow. Therefore, the fluid pressure in the drain line 37 upstream of the operational one-way check valve 300 becomes higher, i.e. higher than the offset pressure P₀. Then, the pressure relief valve 207 becomes active to open for allowing the excessive pressure of the working fluid to flow through the by-pass line 210.

When the engine stops, the pressure unit 16 ceases operation. By stopping the pressure unit 16, the working fluid pressure in the supply line 35 drops. According to drop of the pressure in the supply line 35, the pilot pressure to be exerted to the operational one-way check valve 300 via the pilot line 300a drops. When the pressure in the pilot line 300a drops below or equal to the set pressure, the operational one-way check valve 300 is switched into operational one-way check position to block fluid communication therethrough. As a result, the fluid pressure in the drain line 37 upstream of the operational one-way check valve 300 becomes equal to the pressure in the working chamber 26d. Therefore, even when the working fluid leaks through a gap between the spool valve 52 and the inner periphery of the valve bore, it is not affect the fluid pressure in the working chamber.

FIG. 4 shows variation of the working fluid pressure in the working chamber 26d of the hydraulic cylinder 26 according to variation of the current value of the control signal applied to the actuator 29 of the pressure control valve 28. As seen from FIG. 4, the hydraulic pressure in the working chamber 26d varies between a maximum pressure P_(max) which is saturation pressure of the pressure source unit 16 and a minimum pressure P_(min) which is set at a magnitude in view of a noise component to be contained in the control signal. As seen from FIG. 4, the maximum pressure P_(max) corresponds to the maximum current value I_(max) of the control signal and the minimum pressure P_(min) corresponds to the minimum current value I_(min) of the control signal. Furthermore, the hydraulic pressure level as labeled P_(N) represents neutral pressure at the neutral current I_(N). As seen, the neutral current I_(N) is set at an intermediate value between the maximum and minimum current values I_(max) and I_(min).

Operation of the aforementioned pressure control valve 28 in terms of control of suspension characteristics and absorption of road shock will be discussed herebelow.

In general, the pressurized working fluid source unit 16 supplies the predetermined line pressure. For example, the line pressure in the supply line 35 may be set at a pressure of 80 kgf/cm².

When the vehicle steadily travels on a smooth straight road, the current value of the control signal to be applied to the actuator 29 of the pressure control valve 28 is maintained at the neutral value I_(N). As long as the neutral value I_(N) of the control signal is applied to the actuator 29, the proportioning solenoid coil 68 is energized at a magnitude corresponding the neutral value I_(N) of the control signal to place the poppet value 48 at the corresponding position. At this position, the flow resistance at the communication path opening 46A, path area of which is restricted by the valve head 48a of the poppet valve 48 becomes the neutral value. At this position of the poppet valve 48, the pilot pressure P_(p) within the pilot chamber PR is maintained at the neutral pressure P_(N). At this condition, if the fluid pressure is the control pressure PC in the pressure control port 54c is held equal to the fluid pressure in the working chamber 26d of the hydraulic cylinder 26, the fluid pressure in the upper and lower feedback chambers FU and FL are held in balance to each other. The valve spool 52 is maintained at the neutral position to shut fluid communication between the supply port 54s, the drain port 54r and the pressure control port 54 c. Therefore, the control pressure PC is maintained at the neutral pressure P_(N).

At this condition, when relatively high frequency and small magnitude road shock input through the vehicular wheel, is absorbed by fluid communication between the working chamber 26d and the pressure accumulator 34 via the orifice 32. The flow restriction in the orifice 32 serves to absorb the bounding and rebounding energy. Therefore, high frequency and small magnitude road shock can be effectively absorbed so as not to be transmitted to the vehicle body.

When the piston 26c strokes in rebounding direction compressing the working chamber 26d, the fluid pressure in the working chamber increases to increase the control pressure Pc in the pressure control port 54c. Therefore, the control pressure Pc becomes higher than the pilot pressure P_(p) in the pilot chamber PR. This results in increasing of the fluid pressure in the lower feedback chamber FL at a magnitude higher than that in the upper feedback chamber FU. This causes upward movement of the valve spool 52 to establish fluid communication between the drain port 54r and the pressure control port 54c. Therefore, the pressure in the pressure control port 54c is drained through the drain line 37. This causes pressure drop at the pressure control port 54c so that the control pressure Pc becomes lower than the pilot pressure P_(p) in the pilot chamber PR. Then, the fluid pressure in the upper feedback chamber FU becomes higher than that in the lower feedback chamber FL. Therefore, the valve spool 52 is shifted downwardly to establish fluid communication between the supply port 54s and the pressure control port 54c. The pressurized working fluid in the supply line 35 is thus supplied to the working chamber 26d via the pressure control port 54c to increase the fluid pressure. By repeating the foregoing cycles, pressure balance is established between the pressure control port 54c and the pilot chamber PR. Therefore, the control pressure Pc as well as the fluid pressure in the working chamber 26d are adjusted to the pilot pressure.

During the pressure adjusting operation set forth above, the fixed throttling orifice Pro serves for restricting fluid flow from the pressure control port 54c to the drain line 37. This flow restriction at the orifice Pro serves as resistance against the rebounding stroke of the piston 26c to damp or absorb energy causing rebounding motion of the vehicle body. Furthermore, as set out, working fluid in the pilot chamber PR is generally introduced through the pilot path PP via the multi-stage orifice Qp and return through the pilot return path PT via the lower section 42Ul of the control chamber 42U and via the multi-stage orifice Pr. As long as the fluid flow in the pilot return path PT is not disturbed and thus steady. The most upstream side orifice of the multi-stage orifice Pr is mainly effective for restricting the fluid flow. Therefore, magnitude of flow restriction is relatively small so as to provide sufficient response characteristics in reduction of the pilot pressure. On the other hand, when the working fluid flowing from the control chamber 42U confluence with the working fluid from the pilot chamber PR, back pressure is produced in the drain port 54r, the fluid flowing through the pilot return path PT is disturbed and thus becomes unstable. This tends to cause serving of the pressurized fluid from the drain port 54r to the pilot chamber PR. In such case, all of the orifices in the multi-stage orifice Pr is effective to create greater flow restriction than that for the steady flow. This avoid influence of the back pressure created in the drain port 54r.

Similarly, in response to the bounding stroke of the piston 26c, the valve spool 52 is shifted up and down to absorb bounding energy and maintains the fluid pressure in the working chamber 26d of the hydraulic cylinder 26 at the neutral pressure.

On the other hand, when the anti-rolling suspension control is taken place in response to the lateral acceleration exerted on the vehicle body, the control signal current value is derived on the basis of the magnitude of the lateral acceleration monitored by the lateral acceleration sensor 23. Generally, in order to suppress rolling motion of the vehicular body, the fluid pressure in the working chamber 26d of the hydraulic cylinder 26 which is provided for the suspension mechanism at the side where the vehicular height is lowered across the neutral position, is increased to suppress lowering motion of the vehicle body. On the other hand, the fluid pressure in the working chamber 26d of the hydraulic cylinder 26 which is provided for the suspension mechanism at the side where the vehicular height is risen across the neutral position, is decreased to suppress rising motion of the vehicle body. Therefore, in order to control the pressure in the working chambers 26d of the both side hydraulic cylinders 26, control signal current values are increased and ceased across the neutral value I_(N).

For example, when rolling motion is caused by left turn of the vehicle, control current for the actuators 29 of the pressure control valves 28 controlling the fluid pressures in the front-right and rear-right hydraulic cylinders 26FR and 26RR are to be increased to be greater than the neutral current I_(N), and the control current for the actuator of the pressure control valves 28 controlling the fluid pressures in the front-left and rear-left hydraulic cylinders 26FL and 26RL are to be decreased to be smaller than the neutral current I_(N). By the control current supplied to respective actuators 29, the proportioning solenoid coils 68 are energized at the magnitudes corresponding to the control signal currents to place the poppet valves 48 at respective corresponding positions. By variation of the positions of the poppet valves 48, flow restriction magnitude at respective communication path openings 46A is varied to vary the pilot pressures P_(p) in the pilot chamber PR. As set forth, since the fluid pressures in the working chambers 26d become equal to the pilot pressures P_(p), the suspension characteristics at respective hydraulic cylinders 26 can be adjusted.

Anti-pitching, bouncing suppressive suspension control can be performed substantially in the same manner to that discussed with respect to the anti-rolling control.

The fluid supply controller 400 is connected to a pump speed sensor 402, a front-left stroke sensor 404 and a front-right stroke sensor 406. The pump speed sensor 402 generally monitors rotation speed of the engine output shaft 200a as a pump revolution speed representative parameter for producing a pump speed indicative signal N. For monitoring rotation speed of the engine output shaft 200a, any of appropriate sensors, such as magnetic, optical pick-up type sensors and so forth can be used. The front-left and front-right stroke sensors 404 and 406 are respectively disposed in the front-left and the front-right suspension systems for monitoring relative strokes between the vehicular body and the suspension member for producing front-left and front-right stroke indicative signals X_(L) and X_(R). The fluid supply controller 400 processes the pump speed indicative signal N and the front-left and front-right stroke indicative signals X_(L) and X_(R) for deriving the flow control signal CS in order to control the valve position.

As shown in FIG. 7, the fluid supply controller 400 comprises band-pass filters 410 and 412 respectively receiving the front-left and front-right stroke indicative signals X_(L) and X_(R) for filtering out the stroke signal in a frequency range out of a predetermined frequency range which is defined by higher and lower cut-off frequencies f_(H) and f_(L). The lower cut-off frequency f_(L) is set at a frequency corresponding to the frequency of vibration caused during vehicular height adjustment. For example, in the shown embodiment, the lower cut-off frequency f_(L) is set at 0.5 Hz. On the other hand, the higher cut-off frequency F_(H) 6 Hz, for removing frequency component corresponding to resonant frequency range of sprung mass constituted of the suspension member, road wheel and so forth. The stroke indicative signals X_(L) and X_(R) are also fed to low-pass filters 430 and 432. These low-pass filters 430 and 432 filter out high level components of the stroke indicative signal and thus extract envelope components. Such high frequency removed envelope of the stroke indicative signals may be equivalent to means value of the stroke indicative signal X_(L) and X_(R). Practically, the cut-off frequency of the low-pass filters 430 and 432 are set at a frequency range corresponding to road shock vibration frequency range (approximately 1-10 Hz). Therefore, the output of the low-pass filters 430 and 432 may serve as mean value signals X_(L) and X_(R), respectively representing the means values of the stroke indicative signals X_(L) and X_(R). The low-pass filters 430 and 432 are respectively connected to adder circuits 434 and 436 for supplying the means value signals X_(L) and X_(R). Also, the stroke indicative signals X_(L) and X_(R) are supplied to the adder circuits 434 and 436. The adder circuits 434 and 436 have non-inverting input terminals for receiving the stroke indicative signals X_(L) and X_(R) and inverting input terminals for receiving the means value signals X_(L) and X_(R). The adder circuits 434 and 436 sum the inputs to derive differences indicative values (X_(L) -X_(L)) and (X_(R) -X_(R)). The adder circuits 434 and 436 supply the difference indicative values to absolute value circuits 438 and 440. The absolute value circuits 438 and 440 derive absolute values |X_(L) -X_(L) | and |X_(R) -X_(R) | which represent magnitude of vertical stroke at front left and front right suspension systems.

Respective band-pass filters 410 and 412 output filtered signal X_(L) ' and X_(R) ' and supply to integrator circuits 414 and 416. Each of the integrator circuits 414 and 416 derives an integrated stroke value Q_(L) and Q_(R) on the basis of the filtered signal values X_(L) ' and X_(R) ' utilizing the following equation: ##EQU1## where Q: Q_(L), Q_(R) ;

X: stroke gradient of each filtered stroke indicating signal value (X_(L) ', X_(R) ');

T: integration period which is set in terms of the steering frequency, switching characteristics of the fluid pumps and so forth; and

K: gain determined corresponding to effective area of the hydraulic cylinder 26

The integrated stroke values Q_(L) and Q_(R) derived by the integrator circuits 414 and 416 are fed to an adder circuit 418. The adder circuit 418 is also connected to a pilot flow rate setting circuit 420 which generates a pilot flow rate indicative value Q₀ representative of total leak fluid amount in the pressure control valves 28. The adder circuit 418 adds the integrated stroke values Q_(L) and Q_(R) and the pilot flow rate indicative value Q₀ for deriving a predicted fluid flow rate indicative value Q_(A).

Here, in the practical vehicular bounding and rebounding activity, bounding motion and rebounding motion generally appears alternatively as illustrated by line x in FIG. 8. For the illustrated variation, the integrated value Q varies with a given phase shift as shown by the line X and represents the hatched areas A and B. As can be seen, increased amount of fluid becomes necessary in the rebounding stroke in the area A. Therefore, as long as the front suspension systems as illustrated in FIG. 8 is concerned, increased amount of fluid is not required in the bounding stroke as represented by the area B.

The fluid supply controller 400 further includes a mode selector circuit 422 which receives the pump speed indicative signal N from the pump speed sensor 402 and the predicted fluid flow rate indicative value Q_(A). The mode selector circuit 422 is also connected to the absolute value circuits 438 and 440 to receive therefrom the vertical stroke magnitude indicative values. The mode selector circuit 422 thus derives a mode selection signal SL representative selected one of the fluid supply mode according to the mode map as illustrated in FIG. 6. Mode selection signal SL is fed to a driver circuit 424 which output the flow control signal CS.

Based on these input data, the mode selector circuit 422 performs mode setting operation according to the process illustrated in FIG. 9. The routine of FIG. 9 is executed at every given time interval. In the shown embodiment, the interval of mode setting operation is set at a length corresponding to the integration period T so that the shown routine can be executed in synchronism with integrating operation in the integrator circuits 414 and 416. On the other hand, the shown routine is executed every given interval, e.g. 20 ms. Immediately after starting execution in each execution cycle, a counter value c is incremented by one (1) at a step 1002. Then, at a step 1004, the counter value c as incremented at the step 1002 is compared with a predetermined value A corresponding to the interval of operation for setting mode. When the counter value c as checked at the step 1004 is smaller than the predetermined value A, process directly goes END and returns to a main or background routine. On the other hand, if the counter value c as checked at the step 1004 is equal to the predetermined value A, then, the counter value c is cleared at a step 1006. Subsequently, the predicted flow rate indicative value Q_(A) is read out at a step 1008, and the pump speed indicative signal value N is read out at a step 1010. Then, at a step 1012, the mode selection among a plurality of fluid flow rate modes as shown in FIG. 6 is performed in order to select a basic flow rate mode on the basis of the predicted flow rate indicative value Q_(A) and the pump speed indicative signal value N. Thereafter, a stroke magnitude dependent flow control state indicative flag a, which is set and reset through the process illustrated in FIG. 10 and will be discussed, is checked whether the flag a is set or not, at a step 1014. When the stroke magnitude dependent flow control state indicative flag a is not set as checked at the step 1014, the basic flow rate mode is set as active flow rate control mode for actually controlling the pump operation, at a step 1016. Subsequently, the mode selection signal SL is output to the driver circuit 424, at a step 1018.

On the other hand, if the counter value C as checked at the step 1004 is not equal to A, the stroke magnitude dependent flow control state indicative flag a is checked whether the flag a is set or not, at a step 1020. When the stroke magnitude dependent flow control state indicative flag a is set as checked at the step 1020, the basic flow rate mode is modified for selecting one level higher flow rate mode for increased pump discharge rate a step 1022. Then, process goes to the step 1018 for outputting the mode selection signal SL. On the other hand, if the stroke magnitude dependent flow rate dependent control state indicative flag a is not set as checked at the step 1020, process directly goes END.

FIG. 10 shows a process for detecting vertical stroke requiring greater fluid flow rate for providing sufficient response characteristics in active suspension control. Immediately after starting execution, the absolute value |X_(R) -X_(R) | supplied from the absolute value circuit 440, which represents vertical stroke magnitude at the front right suspension system is read out, at a step 1102. Similarly, at a step 1104, the the absolute value |X_(L) -X_(L) | supplied from absolute value circuit 438, which represents vertical stroke magnitude at the front left suspension system is read out. Then, the absolute value |X_(R) -X_(R) | is compared with a predetermined stroke criterion E at a step 1106. The same check is also performed for the absolute value |X_(L) -X_(L) |, at a step 1108. When the vertical stroke magnitude greater than the stroke criterion is detected in either of the steps 1106 and 1108, a stroke indicative parameter value f_(i) is set at one (1) at a step 1110. Then, at a step 1112, the stroke indicative parameter value f_(i) set at the step 1110 in the current execution cycle and f_(i-1) set in the immediately preceding execution cycle are checked. When the stroke indicative parameter value f_(i) is set at one (1) which value represents large stroke magnitude, and the stroke indicative parameter value f_(i-1) is set at zero (0) which value represents small stroke magnitude, a counter value d is incremented by one (1) at a step 1114. Then, the stroke magnitude dependent flow control state indicative flag a is checked at a step 1116. If the stroke magnitude dependent flow control state indicative flag a is not set as checked at the step 1116, the flag is set at a step 1118.

On the other hand, when both answer at the steps 1106 and 1108 are negative, the stroke indicative parameter value f_(i) is set at zero (0) at a step 1120. Thereafter, the stroke magnitude dependent flow control state indicative flag a and the counter value d are checked at a step 1122. When the stroke magnitude dependent flow control state indicative flag a is set at one (1) and the counter value d is equal to or greater than one (1), as checked at the step 1122, further check is performed for the stroke magnitude dependent flow control state indicative flag a and the counter value d, at a step 1124. When the stroke magnitude dependent flow control state indicative flag a is set at one (1) and the counter value d is equal to two (2), as checked at the step 1124, a flag e is checked at a step 1126, which flag represents the states that the vertical stroke is maintained in large magnitude or an elapsed time after termination of the large stroke magnitude is shorter than a predetermined period, is checked, at a step 1126. When the flag e as checked at the step 1126 is not set as checked, a counter value b is cleared and the flag e is set, at a step 1128.

At a step 1130, the counter value c is checked whether the counter value is zero. If the counter value c as checked at the step 1130 is zero, then, the counter value b is incremented by one (1) at a step 1132. Subsequently, the counter value b is checked at a step 1134 whether the incremented counter value b is equal to two (2). If the counter value b as checked at the step 1134 is equal to two, then, the flags a and e are reset and the counter values b and c are cleared at a step 1136.

After the process at either the step 1118 or 1136, the stroke indicative prameter data f_(i-1) as the previously derived parameter data is update by the current one f_(i) at a step 1138.

On the other hand, if the anser at the step 1122 is negative process directly jumps to the step 1136. Similarly, if the answers at the step 1124 is negative or the answer at the step 1126 is positive, process jumps to the step 1130. If the counter value c is not zero as checked at the step 1130 or is counter value b is not two as checked at the step 1134, process jumps to the step 1138.

In practice, the controller 400, when the ignition switch is held ON position to maintain the engine running in idling state, the front-left and front-right suspension systems are maintained in static state. Therefore, the front-left and front-right stroke indicative signals X_(L) and X_(R) of the front-left and front-right stroke sensors 404 and 406 are maintained substantially at constant value. Therefore, the frequency of these front-left and front-right stroke indicative signals X_(L) and X_(R) are maintained lower than the lower cut-off frequency. As a result, the output level of the band-pass filters 410 and 412 are held substantially zero (0). Therefore, the predicted fluid flow rate indicative value Q_(A) derived by the adder circuit 418 becomes essentially or approximately equal to the pilot flow rate indicative value Q₀. Then, the point on the mode selection map of FIG. 6 corresponds to the point m₀. At the same time, since the vehicular body attitude is maintained substantially in stable state, the absolute values |X_(R) -X_(R) | and |X_(L) -X_(L) | are both maintained substantially zero. Therefore, the smaller flow rate mode is selected.

In the practical implementation, when the smaller flow rate mode is selected, the flow control signal CS is maintained low level to maintain the solenoid 206d deenergized. At this position, the fluid communication between the first inlet port 206a and the outlet port 206c is established so that the fluid discharged from the second pump 16_(Qb) is supplied through the supply line 35.

On the other hand, when the vehicle travels on a well surfaced smooth road, the road shock vibration with vibration frequency higher than the upper cut-off frequency is removed from the front-left and front-right stroke indicative signals X_(L) and X_(R) by the band-pass filters 410 and 412. Therefore, similar to that in the engine idling state, the front-left and front-right stroke indicative signals X_(L) and X_(R) of the front-left and front-right stroke sensors 404 and 406 are maintained substantially at constant value. Therefore, the frequency of these front-left and front-right stroke indicative signals X_(L) and X_(R) are maintained lower than the lower cut-off frequency. As a result, the output level of the band-pass filters 410 and 412 are held substantially zero (0). Therefore, the predicted fluid flow rate indicative value Q_(A) derived by the adder circuit 418 becomes essentially or approximately equal to the pilot flow rate indicative value Q₀. Then, the point on the mode selection map of FIG. 6 corresponds to the point m₀. Similarly to the above, at this time, since the vehicular body attitude is maintained substantially in stable state, the absolute values |X_(R) -X_(R) | and |X_(L) -X_(L) | are both maintained substantially zero. Therefore, the smaller flow rate mode is selected.

When the vehicle travels on a rough or undulated road, the relative displacement between the vehicle body and the suspension member becomes substantial. If the vertical vibration is caused at relatively high speed, the front-left and front-right stroke indicative signals X_(L) and X_(R) falling within the predetermined frequency range is increased to increase the predicted fluid flow rate indicative value Q_(A). Assuming the point identified by the predicted fluid flow rate indicative value Q_(A) and the pump speed indicative signal value N corresponds to the point m₂ on FIG. 6, the greater flow rate mode is selected. Therefore, the mode selection signal SL commanding the greater flow rate mode is fed to the driver circuit 424. The driver circuit 424 thus output the high level flow control signal CS to energize the solenoid 206d. Therefore, the flow control valve 206 establishes fluid communication between the second inlet port 206b and the outlet port 206c so as to establish direct connection between the second pump 16_(Qb) and the fluid reservoir 16a. At this position, the greater amount of fluid discharged from the first fluid pump 16_(Qa) is supplied to the pressure control valve.

On the other hand, when the undulation on the road surface is not rough enough to cause vertical acceleration greater than the acceleration criterion, the stroke dependent pump control is still effective for controlling the fluid flow rate depending upon the magnitude of vertical stroke. The activity of vertical stoke dependent discharge rate control may be understood from the following discussion given with reference to FIG. 11. In the chart of FIG. 11, it is assumed that the relatively large magnitude of vertical vibration is initiated at a time t₁ and increased across the stroke at a time t₁₁. Until the time t₁₁, since the absolute values |X_(R) -X_(R) | and |X_(L) -X_(L) | are maintained at a value smaller than the stroke criterion. Therefore, the flag a is maintained at reset condition. At the time t₁₁, the flag a is set initially. Then, fluid flow mode is switched from smaller flow rate mode to greater flow rate mode. At a time t₁₂, the stroke magnitude represented by (X_(R) -X_(R)) and (X_(L) -X_(L)) becomes smaller than the stroke criterion. Subsequently, the vertical stroke in the opposite direction becomes excess of the stroke criterion at a time t₁₃. As long as the interval between the times t₁₂ and t₁₃ is shorter than the predetermined period T_(F), the greater flow rate mode is maintained.

It should be noted that when the vertical stroke magnitude becomed excessive for absorbing vibration energy by the action of the valve spool in the pressure control valve in the aid of the increased fluid flow rate, then, the control unit 22 starts bouncing control for suppressing vertical stroke by adjustment of the fluid pressure in the working chamber of the hydraulic cylinder.

FIG. 12 is a diagram of another embodiment of a hydraulic circuit to be employed in the preferred embodiment of an active suspension system according to the present invention. The shown embodiment is differentiated only in the construction of the electromagnetic flow control valve 500. The shown flow control valve 500 is operable in three different modes. Namely, the flow control valve 500 is operable to additional mode position in addition to mode positions of the flow control valve 206 in the former embodiment, in which additional mode position, both of the branched supply lines 35a and 35b are blocked from fluid communication with drain line 37 via the flow control valve. Therefore, in the shown embodiment, the operational mode in which the fluid communication between the branched supply line 35a and the drain line 37 via the flow control valve 500 will be referred to as "minimum flow rate mode", in which both of the fluid communication between the branched supply line 35a and the drain line 37 and between the branched supply line 35b and the drain line 37 via the flow control valve 500, will be referred to as 37 maximum flow rate mode", and in which the fluid communication between the branched supply line 35b and the drain line 37 via the flow control valve is established, will be referred to as "medium flow rate position".

In order to establish the aforementioned three mode positions, the flow control valve 500 is associated with a pair of electromagnetic solenoid 502 and 504. For the solenoid 502, a first flow control signal CS₁ is supplied. On the other hand, for the solenoid 504, a second flow control signal CS₂ is supplied. When the first control signal CS₁ is HIGH level and the second control signal CS₂ is LOW level, the maximum flow rate mode is established. ON the other hand, when the both of the first and second flow control signals CS₁ and CS₂ are held LOW level, the medium flow rate mode position is established. Similarly, when the first control signal CS₁ is LOW level and the second flow control signal CS₂ is HIGH level, the minimum flow rate mode position is established.

For providing the first and second flow control signals CS₁ and CS₂, the mode selector circuit 422 in the fluid supply controller 400 is modified from that in the former embodiment. As can be seen, the mode selector circuit 422 is connected to first and second driver circuits 424a and 424b, as shown in FIG. 13. The mode selector circuit 422 selects one of the aforementioned three modes on the basis of the pump speed N and the predicted fluid flow rate indicative value Q_(A) according to the characteristics of FIG. 14. For this reason, the mode selector circuit 422 receives the pump speed indicating signal value N, the predicted fluid flow rate indicating signal value Q_(A), and the absolute values |X_(L) -X_(L) | and |X_(R) -X_(R) |. The mode selector circuit 422 outputs first and second mode selection signals SL₁ and SL₂ combination thereof representative of the selected mode. The mode selector signal SL₁ is fed to the first driver circuit 424a so that the flow control signal CS₁ output therefrom can be switched between HIGH and LOW level according to the signal level of the mode selection signal SL₁. Similarly, the mode selector signal SL₂ is fed to the second driver circuit 424b so that the flow control signal CS₂ therefrom can be switched between HIGH and LOW level according to the signal level of the second mode selection signal.

FIGS. 15 and 16 are similar routine to those in FIGS. 9 and 10 and are executed in the second embodiment of the hydraulic circuit. Immediately after starting execution in each execution cycle, a counter value c is incremented by one (1) at a step 1002. Then, at a step 1004, the counter value c as incremented at the step 1002 is compared with a predetermined value A corresponding to the interval of operation for setting mode. When the counter value c as checked at the step 1004 is smaller than the predetermined value A, process directly goes END and returns to a main or background routine. On the other hand, if the counter value c as checked at the step 1004 is equal to the predetermined value A, then, the counter value c is cleared at a step 1006. Subsequently, the predicted flow rate indicative value Q_(A) is read out at a step 1008, and the pump speed indicative signal value N is read out at a step 1010. Then, at a step 1012, the mode selection among a plurality of fluid flow rate modes as shown in FIG. 6 is performed in order to select a basic flow rate mode on the basis of the predicted flow rate indicative value Q_(A) and the pump speed indicative signal value N. Thereafter, a stroke magnitude dependent flow control state indicative flag a₁, which is set and reset through the process illustrated in FIG. 10 and will be discussed, is checked whether the flag a₁ is set or not, at a step 1030. When the stroke magnitude dependent flow control state indicative flag a₁ is not set as checked at the step 1030, further check is performed whether another stroke magnitude dependent flow control state indicative flag a₂ is set, at a step 1031. When the stroke magnitude dependent flow control state indicative flag a₂ is not set as checked at the step 1031, basic flow rate mode is set as active flow rate control mode for actually controlling the pump operation, at a step 1032. Subsequently, the mode selection signal SL is output to the driver circuit 424, at a step 1018.

On the other hand, if the counter value C as checked at the step 1004 is not equal to A, the stroke magnitude dependent flow control state indicative flag a₁ is checked whether the flag a₁ is set or not, at a step 1036. When the stroke magnitude dependent flow control state indicative flag a₁ is set as checked at the step 1036, the basic flow rate mode is modified for selecting one level higher flow rate mode for increased pump discharge rate. Then, process goes to the step 1018 for outputting the mode selection signal SL. On the other hand, if the stroke magnitude dependent flow rate dependent control state indicative flag a₁ is not set as checked at the step 1004, the stroke magnitude dependent flow control state indicative flag a₂ is checked whether the flag a₁ is set or not, at a step 1038. When the stroke magnitude dependent flow control state indicative flag a₂ is set as checked at the step 1038, the basic flow rate mode is modified for selecting two level higher flow rate mode for increased pump discharge rate at a step 1034. Similarly, when the stroke magnitude dependent flow control state indicative flag a₂ is set as checked at the step 1031, process goes to the step 1034. Then, process goes to the step 1018 for outputting the mode selection signal SL. On the other hand, if the stroke magnitude dependent flow rate dependent control state indicative flag a₂ is not set as checked at the step 1038, process directly goes END.

FIG. 16 shows a process for detecting vertical stroke requiring greater fluid flow rate for providing sufficient response characteristics in active suspension control. Immediately after starting execution, the the absolute value |X_(R) -X_(R) | supplied from the absolute value circuit 440, which represents vertical stroke magnitude at the front right suspension system is read out, at a step 1102. Similarly, at a step 1104, the absolute value |X_(L) -X_(L) | supplied from the absorlute value circuit 438, which represents vertical stroke magnitude at the front left suspension system is read out. Then, the absolute value |X_(R) -X_(R) | is checked if it is greater than or equal to a predetermined stroke criterion E₂ at a step 1140. The same check is also performed for the absolute value |X_(L) -X_(L) |, at a step 1142. When the vertical stroke magnitude greater than the stroke criterion is detected in either of the steps 1140 and 1142, a stroke indicative parameter value f_(i) is set at one (1) at a step 1144. Then, at a step 1146, the stroke indicative parameter value f_(i) set at the step 1144 in the current execution cycle and f_(i-1) set in the immediately preceding execution cycle are checked. When the stroke indicative parameter value f_(i) is set at one (1) which value represents large stroke magnitude, and the stroke indicative parameter value f_(i-1) is set at zero (0) which value represents small stroke magnitude, a counter value d is incremented by one (1) at a step 1148. Then, the stroke magnitude dependent flow control state indicative flag a₂ is checked at a step 1150. If the stroke magnitude dependent flow control state indicative flag a₂ is not set as checked at the step 1150, the flag is set at a step 1152.

On the other hand, when both answer at the steps 1140 and 1142 are negative, the absolute value |X_(R) -X_(R) | is again checked if it is greater than or equal to or greater than a predetermined stroke criterion E₁ at a step 1154. The same check is also performed for the absolute value |X_(L) -X_(L) |, at a step 1156. When the vertical stroke magnitude greater than the stroke criterion is detected in either of the steps 1154 and 1156, a stroke indicative parameter value f_(i) is set at one (1) at a step 1158. Then, at a step 1160, the stroke indicative parameter value f_(i) set at the step 1158 in the current execution cycle and f_(i-1) set in the immediately preceding execution cycle are checked. When the stroke indicative parameter value f_(i) is set at one (1) which value represents large stroke magnitude, and the stroke indicative parameter value f_(i-1) is set at zero (0) which value represents small stroke magnitude, a counter value d is incremented by one (1) at a step 1162. Then, the stroke magnitude dependent flow control state indicative flag a₁ is checked at a step 1164. If the stroke magnitude dependent flow control state indicative flag a₁ is not set as checked at the step 1164, the flag is set at a step 1166.

On the other hand, when both answer at the steps 1154 and 1156 are negative, the stroke indicative parameter value f_(i) is set at zero (0) at a step 1168. Thereafter, the stroke magnitude dependent flow control state indicative flag a₁ or a₂ and the counter valuer d are checked at a step 1170. When the stroke magnitude dependent flow control state indicative flag a₁ or a₂ is set at one (1) and the counter value d is equal to one (1), as checked at the step 1170, further check is performed for the stroke magnitude dependent flow control state indicative flag a₁ or a₂ and the counter value d, at a step 1172. When the stroke magnitude dependent flow control state indicative flag a is set at one (1) and the counter value d is equal to two (2), as checked at the step 1172, a flag e is checked at a step 1174, which flag represents the states that the vertical stroke is maintained in large stroke magnitude or an elapsed time after termination of the large stroke magnitude is shorter than a predetermined period, is checked, at a step 1174. When the flag e as checked at the step 1174 is not set as checked, a counter value b is cleared and the flag e is set, at a step 1178.

At a step 1180, the counter value c is checked whether the counter value is zero. If the counter value c as checked at the step 1180 is zero, then, the counter value b is incremented by one (1) at a step 1182. Subsequently, the counter value b is checked at a step 1184 whether the incremented counter value b is equal to two (2). If the counter value b as checked at the step 1184 is equal to two, then, the flags a and e are reset and the counter values b and d are cleared at a step 1186.

After the process at either the step 1152, 1166 or 1186, the stroke indicative prameter data f_(i-1) as the previously derived parameter data is update by the current one f_(i) at a step 1138.

On the other hand, if the answer at the step 1170 is negative process directly jumps to the step 1186. Similarly, if the answers at the step 1172 is negative or the answer at the 1174 is positive, process jumps to the step 1180. If the counter value c is not zero as checked at the step 1180 or is counter value b is not two as checked at the step 1184, process jumps to the step 1138.

FIGS. 17 and 18 are modified routine of those in FIGS. 15 and 16 and are executed in the second embodiment of the hydraulic circuit. Immediately after starting execution in each execution cycle, a counter value c is incremented by one (1) at a step 1002. Then, at a step 1004, the counter value c as incremented at the step 1002 is compared with a predetermined value A corresponding to the interval of operation for setting mode. When the counter value c as checked at the step 1004 is smaller than the predetermined value A, process directly goes END and returns to a main or background routine. On the other hand, if the counter value c as checked at the step 1004 is equal to the predetermined value A, then, the counter value c is cleared at a step 1006. Subsequently, the predicted flow rate indicative value Q_(A) is read out at a step 1008, and the pump speed indicative signal value N is read out at a step 1010. Then, at a step 1142, a correction value B which is derived through the process of FIG. 18 and will be discussed later, is read out. Then, the predicted flow rate indicative value Q_(A) is modified with the correction value B to derive a modified predicted value Q_(AA), at a step 1144. Then, the fluid flow rate mode is selected on the basis of the predicted flow rate indicative value Q_(AA) and the pump speed indicative signal value N at a step 1146. Subsequently, the mode selection signal SL is output to the driver circuit 424, at a step 1018.

On the other hand, if the counter value C as checked at the step 1004 is not equal to A, the stroke magnitude dependent flow control state indicative flag a is checked whether the flag a is set or not, at a step 1020. When the stroke magnitude dependent flow control state indicative flag a is set as checked at the step 1020, the process goes to the step 1142. Otherwise process goes END.

FIG. 18 shows a process for detecting vertical stroke requiring greater fluid flow rate for providing sufficient response characteristics in active suspension control. Immediately after starting execution, the absolute value |X_(R) -X_(R) | supplied from the absolute value circuit 440, which represents vertical stroke magnitude at the front right suspension system is read out, at a step 1102. Similarly, at a step 1104, the the absolute value |X_(L) -X_(L) | supplied from the absorlute value circuit 438, which represents vertical stroke magnitude at the front left suspension system is read out. Then, the absolute value |X_(R) -X_(R) | is compared with a predetermined stroke criterion E at a step 1106. The same check is also performed for the absolute value |X_(L) -X_(L) |, at a step 1108. When the vertical stroke magnitude greater than the stroke criterion is detected in either of the steps 1106 and 1108, a stroke indicative parameter value f_(i) is set at one (1) at a step 1110. Then, at a step 1112, the stroke indicative parameter value f_(i) set at the step 1110 in the current execution cycle and f_(i-1) set in the immediately preceding execution cycle are checked. When the stroke indicative parameter value f_(i) is set at one (1) which value represents large stroke magnitude, and the stroke indicative parameter value f_(i-1) is set at zero (0) which value represents small stroke magnitude, a counter value d is incremented by one (1) at a step 1114. Then, the stroke magnitude dependent flow control state indicative flag a is checked at a step 1116. If the stroke magnitude dependent flow control state indicative flag a is not set as checked at the step 1116, the flag is set at a step 1118. After the process at the step 1118, the correction value B is set at a fixed value B₀ at a step 1188.

As can be seen from FIG. 19, the fixed value B₀ is set at a value smaller than variation range of the fluid flow rate so that when correction of the predicted flow rate is made at points m₁ and m₃, selection of higher level flow rate cannot be made.

On the other hand, when both answers at the steps 1106 and 1108 are negative, the stroke indicative parameter value f_(i) is set at zero (0) at a step 1120. Thereafter, the stroke magnitude dependent flow control state indicative flag a and the counter valuer d are checked at a step 1122. When the stroke magnitude dependent flow control state indicative flag a is set at one (1) and the counter value d is equal to or greater than one (1), as checked at the step 1122, further check is performed for the stroke magnitude dependent flow control state indicative flag a and the counter value d, at a step 1124. When the stroke magnitude dependent flow control state indicative flag a is set at one (1) and the counter value d is equal or greater than to two (2), as checked at the step 1124, a flag e is checked at a step 1126, which flag represents the states that the vertical stroke is maintained in large stroke magnitude or an elapsed time after termination of the large stroke magnitude is shorter than a predetermined period, is checked, at a step 1126. When the flag e as checked at the step 1126 is not set as checked, a counter value b is cleared and the flag e is set, at a step 1128.

At a step 1130, the counter value c is checked whether the counter value is zero. If the counter value c as checked at the step 1130 is zero, then, the counter value b is incremented by one (1) at a step 1132. Subsequently, the counter value b is checked at a step 1134 whether the incremented counter value b is equal to two (2). If the counter value b as checked at the step 1134 is equal to two, then, the flags a and e are reset and the counter values b and d and the correction value B are cleared at a step 1136.

After the process at either the step 1188 or 1136, the stroke indicative parameter data f_(i-1) as the previously derived parameter data is update by the current one f_(i) at a step 1138.

On the other hand, if the answer at the step 1122 is negative process directly jumps to the step 1136. Similarly, if the answers at the step 1124 is negative or the answer at the 1126 is positive, process jumps to the step 1130. If the counter value c is not zero as checked at the step 1130 or is counter value b is not two as checked at the step 1134, process jums to the step 1138.

As can be appreciated herefrom, the present invention fulfills all of the objects and advantages sought therefor.

While the present invention has been disclosed in terms of the preferred embodiment in order to facilitate better understanding of the invention, it should be appreciated that the invention can be embodied in various ways without departing from the principle of the invention. Therefore, the invention should be understood to include all possible embodiments and modifications to the shown embodiments which can be embodied without departing from the principle of the invention set out in the appended claims. 

What is claimed is:
 1. A fluid supply system for an active suspension system for supplying fluid pressure for a hollow working cylinder via a pressure control valve for adjusting suspension characteristics in order to suppress a vehicular body attitude change of an automotive vehicle and absorb road shock vibration, said system comprising:a pressurized fluid source unit for circulating pressurized fluid through a fluid circuit extending via said pressure control valve and said working cylinder; sensor means for monitoring a relative displacement between a vehicular body and a suspension member rotatably supporting a road wheel for producing a relative displacement magnitude indicative signal; first means for deriving a predicted fluid flow amount through said fluid circuit on the basis of said relative displacement magnitude indicative signal to produce a predicted fluid flow amount indicative signal; second means for determining on the basis of said relative displacement magnitude indicative signal whether a magnitude of relative displacement is greater than or equal to a predetermined stroke criterion, so as to produce a large stroke indicative signal when said relative displacement magnitude is greater than or equal to said predetermined stroke criterion; and third means for deriving an amount of fluid supplied from said pressurized fluid source unit on the basis of said predicted fluid flow amount for controlling said pressurized fluid source unit in such a manner as to adjust an amount of fluid flow supplied from said pressurized fluid source unit towards the fluid flow amount derived by said third means, said third means being responsive to said large stroke indicative signal for increasing the derived fluid flow amount.
 2. A fluid supply system as set forth in claim 1, wherein said third means maintains the increased fluid flow amount for a given period of time after termination of said large stroke indicative signal.
 3. A fluid supply system as set forth in claim 2, wherein said second means includes a first arithmetic circuit for deriving a mean value of said relative displacement magnitude indicative signal and a second arithmetic circuit for deriving an absolute value of a difference between said mean value and said relative displacement indicative signal and said second means produces said large stroke indicative signal when the absolute value of said difference is greater than said stroke criterion.
 4. A fluid supply system as set forth in claim 2, wherein said second means includes a low-pass filter for extracting a predetermined frequency range of signal component in said relative displacement magnitude indicative signal and an arithmetic circuit for deriving an absolute value of a difference between said extracted signal level and the signal level of said relative displacement magnitude indicative signal for producing said large stroke indicative signal when the absolute value of said difference is greater than said stroke criterion.
 5. A fluid supply system as set forth in claim 3, wherein said fluid circuit includes a supply line for supplying the pressurized fluid to said pressure control valve and a drain line for recirculating the pressurized fluid to said pressurized fluid source unit, and said pressurized fluid source unit including a by-pass line connecting between said supply line and said drain line by-passing said pressure control valve and a flow control valve means disposed within said by-pass line for adjusting pressurized fluid recirculation rate through said by-pass line so as to adjust an amount of fluid flow supplied to said pressure control valve towards said derived fluid flow amount.
 6. A fluid supply system as set forth in claim 5, wherein said pressurized fluid source unit comprises a first pump having a first greater discharge rate and a second pump having a second smaller discharge rate, said flow control valve means selectively connect said first and second pump to said drain line via said by-pass line.
 7. A fluid supply system as set forth in claim 6, wherein both of said first and second pumps have a driven connection with an internal combustion engine of said automotive vehicle.
 8. A fluid supply system as set forth in claim 7, wherein a fluid discharge volume from each of said first and second pumps is variable depending upon an engine speed of said internal combustion engine.
 9. A fluid supply system as set forth in claim 8, which further comprises a pump speed sensor for monitoring a pump speed to produce a pump speed indicative signal, and said third means derives the amount of fluid supplied from said pressurized fluid source unit on the basis of said predicted fluid flow amount and said pump speed monitored by said pump speed sensor.
 10. A fluid supply system as set forth in claim 2, wherein said sensor means comprises a stroke sensor for monitoring a relative stroke between the vehicular body and the suspension member in bounding and rebounding activity of the vehicle so as to produce a stroke indicative signal.
 11. A fluid supply system as set forth in claim 10, wherein said first means extracts a predetermined frequency range of signal component in said stroke indicative sinal such that said first means processes the extracted signal component in order to derive said predicted fluid flow amount.
 12. A fluid supply system as set forth in claim 11, wherein said first means includes a band-pass filter having a predetermined pass band corresponding to said predetermined frequency range.
 13. A fluid supply system as set forth in claim 1, which further comprises a pump speed sensor for monitoring a revolution speed of a pump incorporated in said pressurized fluid source unit to produce a pump speed indicative signal, and said third means derives the amount of fluid supplied from said pressurized fluid source unit on the basis of said predicted fluid flow amount and said pump speed monitored by said pump speed sensor and modifies the fluid amount supplied from said pressurized fluid source unit at a given rate in response to said large stroke indicative signal.
 14. A fluid supply system as set forth in claim 13, wherein said third means selects basic discharge characteristics of said pump on the basis of said predicted fluid flow amount and said pump speed and modifies the discharge characteristics in response to said large stroke indicative signal.
 15. A fluid supply system for an active suspension system including a fluid pressure operated cylinder disposed between a vehicle body and a suspension member rotatably supporting a road wheel and a pressure control valve for adjusting fluid pressure in said cylinder in response to a change in a vehicle body attitude of an automotive vehicle so as to suppress the vehicular body attitude change, comprising:a variable discharge pump unit for circulating pressurized fluid through a fluid circuit extending via said pressure control valve and said cylinder, said pump having a plurality of discharge modes for the pressurized fluid supplied therefrom; a stroke sensor for monitoring a relative displacement between the vehicle body and the suspension member, for producing a relative displacement magnitude indicative signal; first means for deriving a predicted fluid flow amount through said fluid circuit on the basis of said relative displacement magnitude indicative signal to produce a predicted fluid flow amount indicative signal; second means for determining on the basis of said relative displacement magnitude indicative signal whether a magnitude of relative displacement is greater than or equal to a predetermined stroke criterion, so as to produce a large stroke indicative signal when said relative displacement magnitude is greater than or equal to said predetermined stroke criterion; a discharge mode selector for selecting one of said discharge modes of said pump on the basis of said predicted fluid flow amount in such a manner as to shift up into a greater discharge mode only when said large stroke indicative signal is produced and said predicted fluid flow amount exceeds the amount of pressurized fluid fed in a current discharge mode of said pump.
 16. A fluid supply system as set forth in claim 15, wherein said discharge mode selector maintains the shifted-up discharge mode of said pump for a given time interval after termination of said large stroke indicative signal.
 17. A fluid supply system as set forth in claim 16, wherein said second means a first arithmetic circuit for deriving a mean value of said relative displacement magnitude indicative signal and a second arithmetic circuit for deriving an absolute value of a difference between said mean value and said relative displacement indicative signal and said second means produces said large stroke indicative signal when the absolute value of said difference is greater than said stroke criterion.
 18. A fluid supply system as set forth in claim 17, wherein said first arithmetic circuit includes a low-pass filter for extracting a predetermined frequency range of signal component in said relative displacement magnitude indicative signal and said second arithmetic circuit includes an adder for deriving a difference between said extracted signal level and the signal level of said relative displacement magnitude indicative signal and an absolute value generating circuit for producing said absolute value. 